When designing the cooling system of modern gas turbines it is important to be able to predict the heat transfer from the hot gas to the walls surrounding the gas path. One flow feature making this rather complicated is the presence of secondary, three-dimensional flow structures, often referred to as horse shoe vortices, which greatly enhance the rate of heat transfer to the endwall, especially in the leading edge region. During the last few years the V2F turbulence model has become increasingly popular due to its ability to account for near-wall damping without use of ad hoc damping functions. The V2F model has also proved to be superior to other RANS methods in many fluid flows where complex flow features are present. In this study n...
The 2D flow around 13 similar stay-vane profiles with different trailing edge geometries is investig...
In this paper we establish a benchmark data set of a generic high-pressure turbine vane generated by...
In this Master thesis, the prediction of the aerodynamic performance on a low pressure turbine outle...
When designing the cooling system of modern gas turbines it is important to be able to predict the h...
In this study three-dimensional simulations of a stator vane passage flow have been performed using ...
When designing the cooling system of modern gas turbines it is important to be able to predict the h...
Computational fluid dynamics is a cornerstone in gas turbine engine design. It is used to optimize s...
The use of the realizability constraint in (v(2)) over bar -f turbulence models is assessed by compu...
In this work, a numerical study has been performed to simulate the heat transfer and fluid flow in a...
Modern gas turbines always operate at a high level of inlet temperature. The current inlet temperatu...
New design goals on modern jet engines often leads to more highly loaded turbines with fewer stages ...
The accurate numerical simulation of the flow through turbine stages strongly depends on the proper ...
The turbine inlet guide vanes of a gas-turbine are subjected to extreme hot gas temperatures which i...
In this paper, we establish a benchmark data set of a generic high-pressure (HP) turbine vane genera...
Accurate predictability of high-pressure turbine nozzle guide vane aero-thermal performance is highl...
The 2D flow around 13 similar stay-vane profiles with different trailing edge geometries is investig...
In this paper we establish a benchmark data set of a generic high-pressure turbine vane generated by...
In this Master thesis, the prediction of the aerodynamic performance on a low pressure turbine outle...
When designing the cooling system of modern gas turbines it is important to be able to predict the h...
In this study three-dimensional simulations of a stator vane passage flow have been performed using ...
When designing the cooling system of modern gas turbines it is important to be able to predict the h...
Computational fluid dynamics is a cornerstone in gas turbine engine design. It is used to optimize s...
The use of the realizability constraint in (v(2)) over bar -f turbulence models is assessed by compu...
In this work, a numerical study has been performed to simulate the heat transfer and fluid flow in a...
Modern gas turbines always operate at a high level of inlet temperature. The current inlet temperatu...
New design goals on modern jet engines often leads to more highly loaded turbines with fewer stages ...
The accurate numerical simulation of the flow through turbine stages strongly depends on the proper ...
The turbine inlet guide vanes of a gas-turbine are subjected to extreme hot gas temperatures which i...
In this paper, we establish a benchmark data set of a generic high-pressure (HP) turbine vane genera...
Accurate predictability of high-pressure turbine nozzle guide vane aero-thermal performance is highl...
The 2D flow around 13 similar stay-vane profiles with different trailing edge geometries is investig...
In this paper we establish a benchmark data set of a generic high-pressure turbine vane generated by...
In this Master thesis, the prediction of the aerodynamic performance on a low pressure turbine outle...